The Influence of Exhaust System on the Performance of the High Bypass Ratio Turbofan Engine Nacelle (AIAA 2018-4669)
Joint propulsion conference
2018-01-01
11 pages
Aufsatz (Konferenz)
Englisch
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Effect of Serpentine Nozzle on Bypass Ratio of Turbofan Engine Exhaust (AIAA 2018-4744)
British Library Conference Proceedings | 2018
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